Ygtjki

Escape velocity for a vertical take-off on Ceres is about 510 m/s with a gravitational resistance of 0.27 m/s and no atmosphere to cause drag, meaning you'd be spending a LOT more fuel just getting up to speeds appropriate for interplanetary travel than you would just getting stuff into deep space. This means that landing a heavy freighter to make loading easier might be more worthwhile than orbiting it and loading it one little shuttle at a time.

You could also maintain an orbit of about ~112 m/s flying at near surface altitudes making point to point transportation around the asteroid practically free; so, you could have a central loading airbase for your freighters that smaller shuttles bring stuff to from around the "globe". My guess is that people would focus more on time efficiency than fuel efficiency meaning flying in straight lines wherever possible would be the ideal way to go.

The #1 reason why I think this would take priority over an orbital loading system is that you can build a large central distribution warehouse much more cheaply on the ground than in orbit, and central distribution is key to profitability. This means that your various mines & refineries can fill up their shuttles and send them to the distribution center whenever they have enough resources to fill them up without having to wait for freighters to show up looking for what they are selling or co-ordinate launch windows. This means you need fewer shuttles that can be kept in transit for more of their time increasing your mining profits. It also makes loading and unloading much safer and faster. A small mess-up in one of the hundred a mid-air dockings it takes to load your freighter could cause a hull breach killing everyone involved. But if you land it, there is only one opportunity for failure. Then once on the ground, cranes can load it much faster than shuttles with way less over head or risk of high speed collisions. Centralization is also is better for the freighter wait times because the distribution center can make sure it has all the right resources queued up and by the landing pad before it gets there. Frankly, there are tons of ways to exploit centralised logistics that probably go outside of the scope of this question, but in the end, you want it, and putting it in space is just too expensive and risky when take-offs and landings are so cheap.

Complex flight planning may still be needed to the point of making sure people don't crash into each other, but by the time we're advanced enough to colonize Ceres, I'm sure AI will be far enough along to automate flight paths and navigation making local flight traffic a bit of a non-issue in the colonists daily lives as long as you have an orbital GPS system, and good topographical data to coordinate everything.

Space Elevators

Ceres's has a "Day" of 9 hours and low mass puts its Cere-stationary orbit about 1800km above its surface. With its weaker gravity of 0.03g's, any number of modern polymers have sufficient strength to simply lower from a stationary orbit to any point on the surface.

Delta-v is naturally a concern but

$Delta_v$ isn't a concern. Escape velocity is ~514m/s, and using a peroxide rocket, a teeny-tiny mass ratio of 1.5 is enough to get you into solar orbit from Ceres' surface (for reference, the spaceshuttle had a mass ratio of 15, and it used engines with more than triple the specific impulse of peroxide). Not that you'd be doing such a thing, because you'd just use an electromagnetic or steam catapult to boost you up instead and use a tiny rocket motor to circularise your orbit. Orbital speed at cererean synchronous altitude is a miniscule ~186m/s so you don't need a whole lot of fuel to boost up and down or out as you wish.

In fact, $Delta_v$ is such a non-issue that it could easily make sense to not bother with your freighters at all, and simply boost stuff into space on an Earth (or wherever) intercept trajectory with a little engine to do mid-course correction and the final destination orbit injection burn. You'd either have to wait for a transfer window to open (which is infrequent, though I don't recall of the top of my head how infrequent) or you just put up with the fact that your cargo will take a few extra years to get home. If it is just dumb matter, that's not exactly a big deal. It is rather boring from a space-traffic-control-story point of view, however.

Your freighters don´t sit in a parking swarm, they land on trains on Ceres. As Ceres is an airless world we needn´t concern ourselves with aerodynamic drag or entry stresses. Yet this is an incidental detail, as the point of using mass-driver trains to launch vessels it to free them to the Tyranny of the Rocket Equation [1]. The Rocket Equation basically says one of three things. The vessel needs to be mostly fuel (current rockets), be efficient and horribly boring (ion drives) or be a torchship [2](which may fall under your restriction of "no super tech" and might be a bit on the dangerous side (Kzinti Lesson) [3]). The mass drivers are still a case for the Kzinti Lesson, but looking at Johns Law [4] that is unavoidable.

The mass drivers will be maglev trains [5] where vessels land on wagons and are pushed up to speed or slowed down. While this takes energy the energy isn´t fully lost if regenerative brakes [6] are used. To power the thing fusion would be nice but messing around with solar panels or fission plants would work, too. It matters that a lot of energy is needed. I´ll come back to that later. If you want to calculate the dimensions of the mass drivers this formula is relevant.

$v = d/sqrt[2](d/(0,5*a))$

$v$ = velocity

$d$ = distance (track length)

$a$ = acceleration

$v$ should at least be at 510 $m/s$, as that is Ceres escape velocity. At the still human tolerable acceleration of 5 $g$ this gives you a track length of ca. 120 km. Play and plug as you like. It should be noted that the logical conclusion of this technology is a track around the equator, setting $d$ to infinite and allowing all kinds of funny high-velocity launching. Furthermore, this will allow Brachistochrone Orbitals [7] which are the opposite of our current Hohmann Transfers [8]. A note on $a$, 5 $g$ seems to be the save human maximum but I would go for 3 $g$ as that is more comfortable. Unmanned vessels could be shot off at hundreds of $g$´s.

With the infrastructure of the spaceports cleared up let´s look at trajectories. Freighters will need to time their flight plans to the rotation of Ceres and need to maneuver to correct their courses in a manner allowing for save capture and beneficial departure. If both target and launch point have mass drivers only ion drives are needed for corrections. If not the mass drivers will still lower fuel demands and be economically viable, especially as using the power directly to launch vessels will be more efficient than producing Hydrogen Peroxide. (tell me in a comment should you want me to run the numbers). Hohman transfers will be dominant during the early phase of colonization, with Brachistochrone Orbitals only possible at certain times and only in the Belt. As mass-driver infrastructure improves the windows for Brachistochrone Orbitals will grow bigger until Hohman Trajectories will be a thing of the past like travel by horse is today. This obviously assumes that you don't have torchships.

As for your shuttle flight paths, there are two things I mentioned earlier that are relevant to this discussion. That running mass-driver takes a lot of energy and that according to you the colonisation of Ceres is in an early state. This leads to the conclusions that there will be few and short mass-drivers on Ceres. Around those the major settlements will grow but what about those far from these spaceports? Here your shuttle pilot comes in. He will pilot one of the many shuttles and thugs carrying people and materials to and from the mass-drivers. Now, why does this shuttle hopping happen? Ceres has a surface area of ca. 2.7 mil $m²$, roughly comparable to Kazakhstan. But the land is mountainous and the ice keeps melting and moving, so installing hyperloop trains [9] will take another century. Even roads are impractical.

As Ceres orbital speed at surface level is only 336 $m/s$ and the fuel is cheap the small vessels will fly extremely low trajectories, those who are risk-conscious a few kilometers high, those who want to cut cost only meters above the highest peaks. This is great story material as figuring out that there isn´t enough fuel to get you over the next mountain and pirates harpooning transport vessels down can create a lot of conflicts. The orbits would spread out like the canopy of a tree from the spaceports. it might be more accurate to call them "Jumps" because this isn't really different from jumping on Earth.

Finally, I would recommend the game "Kerbal Space Programm" [10] to you as it will allow you to get an intuitive understanding of orbital mechanics and delivers you the feel of being a spacefarer.

[1] https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation

[2] http://www.projectrho.com/public_html/rocket/torchships.php

[3] http://www.projectrho.com/public_html/rocket/spacegunexotic.php#propulsion

[4] http://www.projectrho.com/public_html/rocket/prelimnotes.php#johnslaw

[5] https://en.wikipedia.org/wiki/Maglev

[6] https://en.wikipedia.org/wiki/Regenerative_brake

[7] http://www.projectrho.com/public_html/rocket/torchships.php#id--Brachistochrone_Equations

[8] https://de.wikipedia.org/wiki/Hohmann-Transfer

[9] https://en.wikipedia.org/wiki/Hyperloop

[10] https://store.steampowered.com/app/220200/Kerbal_Space_Program/

Besides a static space elevator, we might also use a crane, or temporary space elevator. Basically a rope from a ship in stationary orbit unloading supplies and loading resources.

Catapulting things into orbit, as mentioned above, would also work. A ship could choose an elliptic orbit to catch the rocks at about the same speed and their highest elevation or or a suitable tangential movement. I'll leave the mathematics to you. It may collect the rocks or mount engines on them which put them onto desired paths and then return for refuelling - maybe after pushing something from another asteroid or moon towards ceres.

 s os
 s xCCCCx o s
 s CCCCCCCCCC o s .
 s CCCCCCCCCCCC o s .
 s CCCCCCCCCCCC o s o
 s CCCCCCCCCCo s o C=Ceres
 s *CCCC* s o s=Ship/Station
 s s o o=Resources

A gravity assist maneuver could put a ship at very slow speeds and synced to the rotation of Ceres very close to the surface - enough to push a large container with very little energy into the holding bay, and to push loads towards Ceres with just some balloons on the outside to cushion the impact. Once the ship is behind Ceres (as seen relativ to it's movement around the sun), gravity would accelerate the ship again, so no significant energy is lost.

 <s
 s
 s
 s xCCCCx
 s <CCCCCCCC<
s <CCCCCCCCCC< s>
s #<CCCCCCCCCC< s >=Direction
 s <CCCCCCCC< s C=Ceres
 s *CCCC* s s=Ship
 s s #=Resources

As Nosajimiki said on his answer:

You could also maintain an orbit of about ~112 m/s flying at near surface altitudes.

That is very slow for our aerospatial standards. Jets within Earth's atmosphere usually fly at around double that speed.

As you increase altitude, orbital speeds decrease. So your smaller vesses could do it like this:

1. Wait for a launch window (with 9h 4m days, wait times should be relatively short).




2. Launch. Match orbital plane during ascent.




3. You should achieve orbit within a handful kilometers of the target ship.




4. At such small distances and with such low orbital speeds, just accelerate towards target and, when getting close, match speed. The path towards the target will be a very open curve.




5. Use RCS thrusters to maneuver and dock.

To land: undock and land as always.